Control System Design and implementation of a Quadrotor Unmanned Aerial Vehicle
In this paper,a method of embedded system with multi-processor is proposed,so as to satisfy the requirement of strong real-time property,high computational performance and multi-task function of the flight control system.In addition,in order to solve the problems of unknown aerodynamic disturbance and weight uncertainties during flight,a hybrid control method based on sliding mode control (SMC) and model referenced adaptive control (MRAC) is proposed.Through the Lyapunov stability analysis,its proved that the controller is stable.Various simulations were performed and several experiments on the quadrotor UAV validate the control strategies.
Quadrotor UAV Embedded System Hybrid control Multi-processor
Dexin Xu Guangchun Li Lu Wang
College of Automation,Harbin Engineering University,Harbin,China
国际会议
太原
英文
749-753
2012-01-13(万方平台首次上网日期,不代表论文的发表时间)